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  • Stuttgart Wind Energy @ Institute of Aircraft Design

    Reduced Order Modeling of Floating Offshore Wind Turbines

    2nd International Summer School on Stochastic Dynamics of Wind Turbines and Wave Energy Absorbers August, 6th - 8th, 2014

    Aalborg University

    Frank Sandner, Stuttgart Wind Energy (SWE) University of Stuttgart/Germany

  • 2 | (58)

    Stuttgart Wind Energy (SWE)

    Measurement & Control: Preview control Wind field

    reconstruction Conceptual Design & Simulation: Floating Wind

    coupled simulations, CFD, model tests

    Validation with measurements (Alpha Ventus)

    [Floatgen]

    [SWE, InnWind.EU] [SWE,Simpack]

    [SWE, NREL] [USTUTT,IAG]

  • Stuttgart Wind Energy @ Institute of Aircraft Design

    Acknowledgements

    The use and re-distribution of the slides is only allowed upon request to the author.

    These slides are partly based on work by Denis Matha, Steffen Raach and David Schlipf. Their contribution is greatly appreciated.

  • 4 | (58)

    Whats in this lecture?

    To get an understanding of the Floating Wind Turbine (FOWT) as a dynamic system and its modeling techniques.

    To get an idea of how to select the appropriate model simplification.

    To set up a first coupled model.

  • 5 | (58)

    Outline

    1. How to numerically model a Floating Offshore Wind Turbine (FOWT)?

    2. Model Applications

    3. How to reduce/simplify the model?

    4. Example: MBS FOWT model Structural model: Newton-Euler Equations Aerodynamic model Hydrodynamic model

    5. Reduced model applications

    6. Conclusions and Takeaways

    [Ideol]

  • 6 | (58)

    How to model a FOWT (in general)? (1)

  • 7 | (58)

    How to model a FOWT (in general)? (2)

    Model features:

    Coupled/uncoupled Static/dynamic Linear/nonlinear Steady/transient Time/frequency domain Frequency range DOFs, involved modes 2D/3D Parametrizable Computational effort/speed

    (real-time?)

  • 8 | (58)

    How to model a FOWT (in general)? (3) Limited overview on existing software/packages/coupled models:

    FAST (NREL) FAST+ORCAFLEX (Orcina) FAST+MLTSIM (Technip) FAST+OPASS (Cener) FAST+UOU (U of Ulsan)

    GH-Bladed (DNV-GL) SIMO-RIFLEX-HAWC2 (DNV-GL, DTU) SIMPACK+HydroDyn

    (Dassault Systmes, USTUTT, NREL) 3DFloat (UMB) HydroGAST (NTUA) WAMSIM (DHI) SWT (LMS-Samcef) DeepLinesWT (Principia) CAST (U of Tokyo) Wavec2Wire (WaveEC)

    Cordle, A., & Jonkman, J. (2011). State of the Art in Floating Wind Turbine Design Tools. In 21st International Offshore and Polar Engineering Conference.

    Code2code comparison: Robertson, A., Jonkman, J., & Musial, W. (2013).

    Offshore Code Comparison Collaboration , Continuation: Phase II Results of a Floating Semisubmersible Wind System. In Proceedings of the EWEA Offshore. Frankfurt.

    Robertson, A., Jonkman, J., Vorpahl, F., Popko, W., Qvist, J., Froyd, L., Heege, A. (2014). Offshore Code Comparison Collaboration Continuation Within Iea Wind Task 30: Phase Ii Results Regarding A Floating Semisubmersible Wind System. In Proceedings of the ASME 2014 33rd International Conference on Ocean, Offshore and Arctic Engineering. San Francisco, USA.

  • 9 | (58)

    Model Applications (1)

    Overview on model applications

    Why do we need reduced/simplified models?

  • 11 | (58)

    Model Applications (2)

    1. Conceptual design: Early stage coupled simulations Parametric studies Fast load simulations

    [Ideol]

    DLC

    Wind Conditions Wave Conditions

    Events PSF Model Wind Speed Model Wave Height Direction

    1.x Power Production

    1.1 NTM Vin < VHub < VOut NSS Hs = E[Hs | VHub] = 0 Normal operation 1.25 1.2

    1.3 ETM Vin < VHub < VOut NSS Hs = E[Hs | VHub] = 0 Normal operation 1.35

    1.4 ECD Vhub=Vr+/- 2m/s, Vout NSS Hs = E[Hs | VHub] = 0 Normal operation 1.35

    1.5 EWS Vin < VHub < VOut NSS Hs = E[Hs | VHub] = 0 Normal operation 1.35

    1.6a NTM Vin < VHub < VOut ESS Hs = 1.09 Hs50 = 0 Normal operation 1.35

    2.x Power production plus occurrence of fault

    2.1 NTM Vhub=Vr , VOut NSS Hs = E[Hs | VHub] = 0 Pitch runaway 1.35

    2.3 EOG Vhub=Vr+/- 2m/s, VOut NSS Hs = E[Hs | VHub] = 0 Loss of load 1.1

    6.x Parked (standing still or idling)

    6.1a EWM VHub = 0.95 V50 ESS Hs = 1.09 Hs50 = 0, 30 Yaw = 0, 8 1.35

    6.2a* EWM VHub = 0.95 V50 ESS Hs = 1.09 Hs50 = 0, 30 -180 < Yaw < 180 1.1

    6.3a EWM VHub = 0.95 V1 ESS Hs = 1.09 Hs1 = 0, 30 Yaw = 0, 20 1.35

    7.x Parked and fault condition

    7.1a EWM VHub = 0.95 V1 ESS Hs = 1.09 Hs1 = 0, 30 Yaw = 0, 8

    1 seized blade 1.1

  • 12 | (58)

    Model Applications (3)

    1. Conceptual design: Early stage coupled dynamic simulations Parametric studies Fast load simulations

    2. Study/understanding of system dynamics:

  • 13 | (58)

    Model Applications (4)

    Turbulent wind Still sea vs. irregular sea

    Motion Loads

  • 14 | (58)

    Model Applications (5)

    1. Conceptual design: Early stage coupled dynamic simulations Parametric studies Fast load simulations

    2. Study/understanding of system dynamics: Controller design Mass dampers Subsystem adaptation (mooring lines,

    secondary elements)

    [Stewart 2012]

  • 15 | (58)

    Model Applications (6)

    1. Conceptual design: Early stage coupled dynamic simulations Parametric studies Fast load simulations

    2. Study/understanding of system dynamics: Controller design Mass dampers Subsystem adaptation

    (mooring lines, secondary elements) 3. Real-time model:

    Software-in-the-loop experiments (Cener, Polimi, UMaine)

    Model-based control, optimal control

    past

    predicted disturbance

    predicted system

    reference

    future

    projected control

    horizon [Schlipf 2013]

  • 16 | (58)

    Model Applications: Summary

    Questions to be answered by the model:

    1. System dynamics or component dynamics (specific effect)?

    2. Coupled or uncoupled dynamics?

    3. Type of analysis: Steady states, modal, or frequency reponse?

    4. Outputs: Displacements, sectional loads, stresses

    5. Postprocessing: Min/Max/Mean/Stdev, etc.

    Constraints:

    1. Availability of data

    2. Computational speed

    3. Parametrization, batch mode

    4. Flexibility of the software, availability of the code

  • 17 | (58)

    How to reduce the FOWT model? (1)

    Structural Model:

    EMBS

    Elastic Multibody system (EMBS) Elastic parts: full FEM or reduced

    MBS

    MBS of rigid bodies Spring-damper couplings

    Reduction

    Modal reduction, CMS (e.g. Craig Bampton Method)

    Krylov subspace, SVD

  • 18 | (58)

    How to reduce the FOWT model? (2)

    EMBS reduction: Project the equations of motion into a smaller space.

    Modal approximation: Spatial loads not considered. Guyan reduction (condensation): Separation of

    Master (external, interface) and Slave (internal, node displacement) coordinates.

    Component mode synthesis (CMS): Identification of component modes. Homogeneous and particular solution to the EQM correction modes.

    Krylov subspace methods: Large sparse systems, TF estimation

    Singular value decomposition (SVD): Energy consideration, identification of system invariants.

    traditional techniques

    modern techniques

    Nowakowski, C., Fehr, J., Fischer, M., & Eberhard, P. (2012). Model Order Reduction in Elastic Multibody Systems using the Floating Frame of Reference Formulation. In MATHMOD. Retrieved from http://seth.asc.tuwien.ac.at/proc12/full_paper/Contribution475.pdf

    Stru

    ctur

    al d

    ynam

    ics

  • 19 | (58)

    Ab = 0.9969 -0.0030 0.0008 -0.0007 -0.0000 -0.0018 0.9801 0.0105 -0.0090 -0.0005 -0.0005 0.0013 0.9899 0.0177 0.0009 -0.0002 0.0058 -0.0162 0.8036 -0.0241 -0.0000 -0.0005 -0.0005 0.0033 0.9913

    How to reduce the FOWT model? (3)

    Singular-value decomposition (SVD):

    Bb = -0.1445 -0.0246 -0.0537 0.0488 -0.0090 -0.0175 -0.0008 -0.0165 -0.0011 0.0001

    Cb = -0.1466 -0.0725 0.0192 -0.0162 -0.0009

    A2 B2

    C2

    [Lecture Notes Kenn Oldham, Umich ME562 2010]

    Stru

    ctur

    al d

    ynam

    ics

  • 20 | (58)

    How to reduce the FOWT model? (4)

    Gyroscopic effect? Frequency range?

    (selection of modes) Extreme or fatigue

    loads?

    Stru

    ctur

    al d

    ynam

    ics

    [SWE, Simpack]

  • 22 | (58)

    How to reduce the FOWT model? (5)

    Aerodynamic Model:

    CFD

    Potential flow

    BEM

    Actuator point

    Model features: Flow model:

    Blade-tower interaction (wake calculation) Blade-vortex interaction Tip loss, dynamic stall, turbulent wake state Unsteady aerodynamics, dynamic inflow, 3D effects

    Wind field model: Turbulence model 3D/2D/1D

    Blade elasticity (also structural model): Flapwise Edgewise Twist

  • 23 | (58)

    How to reduce the FOWT model? (6)

    [Buelk12]

    [IAG]

    [Wind Energy Handbook]

    Aer

    odyn

    amic

    s

    3 2

    ,1

    2

    p

    a rel

    cM R v

    CFD Lifting line & free wake vortex method

    A